Quote from: Jim on 05/21/2014 02:51 amQuote from: mlindner on 05/21/2014 02:36 amBut most of the volume. Fiberglass has very low density. That makes the requirement for the structure which is most of the mass. Electronics get smaller and System on a Chip (SoC) designs start reducing the volume.Edit: Or actually, more likely is that satellites stay fixed size and get more capable because the marginal cost of X more fuel isn't much once you have the launch of an ELV. We need some cheap microsat/nanosat launchers.again, it isn't the electronics. Microsats and nanosats can't be comsats. The comm package where the mass is. The difference between a laptop and smartphone in terms of electronics would have little effect on the mass or size of a comsat.Well then Jim, looks like we should all just agree to disagree on this point. We'll come back in ten years and see who's argument was closer to the reality we see then.
Quote from: mlindner on 05/21/2014 02:36 amBut most of the volume. Fiberglass has very low density. That makes the requirement for the structure which is most of the mass. Electronics get smaller and System on a Chip (SoC) designs start reducing the volume.Edit: Or actually, more likely is that satellites stay fixed size and get more capable because the marginal cost of X more fuel isn't much once you have the launch of an ELV. We need some cheap microsat/nanosat launchers.again, it isn't the electronics. Microsats and nanosats can't be comsats. The comm package where the mass is. The difference between a laptop and smartphone in terms of electronics would have little effect on the mass or size of a comsat.
But most of the volume. Fiberglass has very low density. That makes the requirement for the structure which is most of the mass. Electronics get smaller and System on a Chip (SoC) designs start reducing the volume.Edit: Or actually, more likely is that satellites stay fixed size and get more capable because the marginal cost of X more fuel isn't much once you have the launch of an ELV. We need some cheap microsat/nanosat launchers.
Quote from: watermod on 05/21/2014 01:15 pmOne of the great mistakes in Iridium was to use movable antennas to talk to the neighboring Iridium sats. The movements changed balance and orbits of the satellites which caused the use of lots of extra fuel to maintain the proper orbit. If they had used phased array antennas to do electronic beam forming instead of moving a physical antenna they would not have used as much fuel to keep their orbit. Over the life of an LEO Iridium sat it could have been a big deal on the mass end of things. So, yeah, modern electronics can make a big difference in the required size.1. How does spacecraft mass properties affect the orbit?2. Phased array antennas would require more power and hence larger solar arrays
One of the great mistakes in Iridium was to use movable antennas to talk to the neighboring Iridium sats. The movements changed balance and orbits of the satellites which caused the use of lots of extra fuel to maintain the proper orbit. If they had used phased array antennas to do electronic beam forming instead of moving a physical antenna they would not have used as much fuel to keep their orbit. Over the life of an LEO Iridium sat it could have been a big deal on the mass end of things. So, yeah, modern electronics can make a big difference in the required size.
So either we are going to see LEO constellations or most of the communication will become terrestrial again with cables as backbones.
So I doubt that in the very long term and assuming the kind of technical evolution you are describing the GEO Comsat market will see such a development towards cheaper, shorter, more.
Well, the problem with GEO is not only cell size, it's also latency. It's too much for good IP based communication. It might be acceptable in those rare cases where you have no other means of access but for everything else it won't be competitive.
So what does this leave GEO? I really don't see that as a growth market in 10 or 15 years, it's a segment you want to cash in on today or never.
Lag Sucks !!!http://wiki.answers.com/Q/What_is_the_Round_Trip_time_of_a_RF_signal_for_GEO_satellitesthe speed of light = 299792458 m / sGEO (Geostationary Earth Orbit) = 35863000 m above the Earth's surfaceround trip time = 2*(35863000)/299792458 =0.239 sthe time needed for an RF signal to reach a GEO satellite and gets retransmitted back to a ground station on earth is approximately 240 milliseconds
Quote from: RocketGoBoom on 05/22/2014 03:01 pmLag Sucks !!!http://wiki.answers.com/Q/What_is_the_Round_Trip_time_of_a_RF_signal_for_GEO_satellitesthe speed of light = 299792458 m / sGEO (Geostationary Earth Orbit) = 35863000 m above the Earth's surfaceround trip time = 2*(35863000)/299792458 =0.239 sthe time needed for an RF signal to reach a GEO satellite and gets retransmitted back to a ground station on earth is approximately 240 millisecondsWhich is quite a lag for games. It is OK for other uses, though. I agree and think that LEO constellations might be better in the future.
No he is not overstating this. Satellite lag from GEO precludes most two-way communications except where terrestrial alternatives are not available (or preferable). This is basically all modern telecommunications except for broadcast and military needs.
No one is going to invest and build a two-way platform to use in GEO when they can do so at lower orbits or using terrestrial alternatives.
Isn't Google experimenting with dirigibles for world-wide data coverage? Affordable launch costs plus mass-produced satellites seems vastly better than airships.
Quote from: sghill on 05/22/2014 02:47 pmNo he is not overstating this. Satellite lag from GEO precludes most two-way communications except where terrestrial alternatives are not available (or preferable). This is basically all modern telecommunications except for broadcast and military needs.Shrug. It's alive and well competing against rural DSL. There's no point arguing about it when we can just look and see people using it, including in the US.The only thing it can really compete against is dialup. We were using it at home in our very rural area until last year, but we jumped ship as fast as we could when 4G service became available. It's alive, but I wouldn't call it well. It's a desperate measure.
All of Juno's spacecraft avionics are in this vault. A reduction in the size on the cards inside it would not have an appreciable affect on the spacecraft size. The mass of a GSO comsat is the payload package (TWTA, receivers, solar arrays and antennas) and the rest of the spacecraft is size to this and not the avionics.
Juno is maybe not the best example, because it has really heavy vault for surviving Jovian radiation. The vault holds both the control system and scientific electronics (i.e. the payload). Smaller cards would have reduced the size and mass of the vault,
The only thing it can really compete against is dialup. We were using it at home in our very rural area until last year, but we jumped ship as fast as we could when 4G service became available.
Quote from: llanitedave on 05/22/2014 05:59 pmThe only thing it can really compete against is dialup. We were using it at home in our very rural area until last year, but we jumped ship as fast as we could when 4G service became available.Good call; but it's hard to see a LEO constellation being competitive with an area that can support 4G service.Cell towers can pick their location. GEO birds can pick their location (somewhat) and choose where they point their antennas. So-called atmospheric satellites will be able to choose where they loiter. But a LEO satellite won't be able to control its ground track. The main issue I'm trying to surface here is that much of the revenue potential for a LEO satellite's ground track will be in areas that are sufficiently densely populated to support a denser communications medium. There are certainly cases that LEO can handle better but it isn't automatically the case that the gap between terrestrial means and GEO will support a huge new satellite constellation.